Bernese GPS Software Version 5.0 - Bernese GNSS Software

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6. Data Preprocessing ------------------------------------------------------------------------ SUMMARY OF EPOCH SOLUTIONS ------------------------------------------------------------------------ NUMBER OF EPOCH SOLUTIONS WITHOUT PROBLEMS: 2879 NUMBER OF EPOCH SOLUTIONS WITH A BIG RMS: 0 NUMBER OF EPOCH SOLUTIONS WITH TOO FEW OBS.: 0 NUMBER OF EPOCH SOLUTIONS WITH "BAD" FLAG: 0 TOTAL NUMBER OF EPOCH SOLUTIONS: 2879 MEAN RMS OF THE EPOCH SOLUTIONS: 0.0084 M MAXIMUM RMS FOR AN EPOCH SOLUTION: 0.0273 M EPOCH: 1271 MAX. CLOCK CORR. FOR AN EPOCH SOLUTION: 0.3300E+08 NS EPOCH: 18 MIN. DEG OF FREEDOM FOR AN EPOCH SOLUTION: 4 EPOCH: 1738 ------------------------------------------------------------------------ The clock jump detected in the baseline with the station Zimmerwald can of course again be seen as a clock event in the preprocessing of the zero-difference observation file. The magnitude of 33 ms corresponds exactly to the clock jump estimated in example 1: ------------------------------------------------------------------------ CYCLE SLIPS ACCEPTED IN THIS RUN ------------------------------------------------------------------------ NUMBER OF SLIPS IN L1: 27 NUMBER OF SLIPS IN L2: 27 NUMB TYP N EPOCH SAT FRQ WLF SLIP FRAC RES.L3 IONOS (M) (M) ------------------------------------------------------------------------ 1 JMP * 18 ALL 1 1 -51988860.000 (EQUIVALENT TO -33. MS) 2 JMP * 18 ALL 2 1 -40510800.000 (EQUIVALENT TO -33. MS) ------------------------------------------------------------------------ Because the correction of cycle slips is switched off when preprocessing zero-difference files this section should only contain JMP-entries (or nothing). The handling of detected clock events is reported in a part of the program output which appears only when preprocessing zero-difference files: ------------------------------------------------------------------------ CLOCK EVENT SUMMARY FOR ZERO-DIFFERENCE FILES ------------------------------------------------------------------------ NUMBER OF CLOCK EVENTS: 1 NUMB EPOCH CLOCK(PHASE) CLOCK(CODE) ACTION ------------------------------------------------------------------------ 1 18 -33000000 NS 988544 NS CYC ------------------------------------------------------------------------ Page 128 AIUB
6.5 Preprocessing Phase Observations The following actions are defined corresponding to the settings in panel “MAUPRP 7: Clock Events” for the handling of clock events: CYC indicates a millisecond-jump that was repaired as a cycle slip, MRK indicates that the corresponding observations are marked because the clock event may bias the common clock estimation from code and phase observations, and AMB reports the setup of a new ambiguity for all satellites because of a clock event. 6.5.8 Extraction (MPRXTR) Program MPRXTR (”Menu>Processing>Program output extraction>Phase preprocessing”) extracts information from the output of the program MAUPRP and produces a summary of the following form: SUMMARY OF THE MAUPRP OUTPUT FILE ********************************* SESS FIL OK? ST1 ST2 L(KM) #OBS. RMS DX DY DZ #SL #DL #MA MAXL3 MIN. SLIP 2620 1 OK DWH1 REYZ 5610 4179 0.027 0.024-0.254 0.208 20 184 13 0.046 35 2620 2 OK DWH1 GOLD 1434 5489 0.016 0.015 0.005-0.108 9 111 12 0.049 28 2620 3 OK HERT ONSA 1046 9133 0.011-0.026 0.158 0.084 8 157 7 0.048 23 ... 2620 70 OK ONSA ZIMJ 1207 9510 0.011 0.065-0.133-0.079 33 117 17 0.046 11 2620 71 OK ONSA PENC 1176 6597 0.013-0.012 0.009-0.073 186 42 4 0.009 6137996 ... 2620 81 OK MSKU SUTH 3444 5442 0.016-0.216 0.021-0.070 49 71 17 0.051 9999780 2620 82 OK SUTH ZAMB 2018 5772 0.015 0.006-0.024 0.138 18 53 9 0.044 18 ------------------------------------------------------------------------------- Tot: 82 2791 5545 0.013 34 77 11 The summary file contains one line per baseline processed. The line starts with the session, a file sequence number, the “OK” flag, the first four characters of the station names, and the length of the baseline. The line continues with some information concerning the epochdifference solution: the number of observations, RMS, baseline change in the Cartesian X, Y, and Z components. The next three fields contain the number of corrected cycle slips, the number of deleted points, and the number of multiple ambiguities. Finally the maximum residual for the ionosphere-free linear combination is given followed by the smallest corrected cycle slip. The last line of the summary gives the number of files, the mean baseline length, the mean number of observations, the mean epoch-difference RMS, the mean number of corrected cycle slips, the mean number of deleted points, and the mean number of multiple ambiguities. The summary listing in the zero-difference case contains the RMS and coordinate corrections from the epoch-difference solution for each individual station. All other parameters are identical to the baseline case. If millisecond-jumps were detected in MAUPRP the events are reported below the main table. If a station or baseline was not successfully cleaned the flag will be different from “OK” and the station/baseline should be removed. Apart from the summary file, MPRXTR may create a deletion list file (in the case of preprocessing baseline files also a new baseline definition file). This file is intended to be used for removing bad observation files in an Bernese GPS Software Version 5.0 Page 129
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Bernese GPS Software Version 5.0 Ed
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Bernese GPS Software Version 5.0 As
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Contents 2.3.6.1 Ionosphere-Free Li
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Contents 6.3.3 Kinematic Stations .
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Contents 9.4.4 Pre-Elimination Opti
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Contents 13.2 How to Correct P1-P2
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Contents 18.3.2 Command Bar . . . .
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Contents 20.4 Description of the Pr
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Contents 22.8.2 Station Abbreviatio
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Contents Page XVI AIUB
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List of Figures 5.1 Flow diagram of
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List of Figures 13.3 P1-C1 code bia
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List of Figures 22.20 Tabular orbit
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List of Tables 12.2 Influences of t
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1. Introduction and Overview • bu
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1. Introduction and Overview Table
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1. Introduction and Overview • Th
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1. Introduction and Overview The Be
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1. Introduction and Overview for Ca
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2. Fundamentals 2.1.1 GPS System De
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2. Fundamentals Table 2.2: Componen
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2. Fundamentals Clock correction [n
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2. Fundamentals Figure 2.5: GLONASS
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2. Fundamentals Table 2.6: GLONASS
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2. Fundamentals In contrast to the
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2. Fundamentals 2.2 GNSS Satellite
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2. Fundamentals 2.2.2.1 The Kepleri
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2. Fundamentals Table 2.9: Perturbi
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2. Fundamentals R.A. of Ascending N
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2. Fundamentals where aROCK is the
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2. Fundamentals By taking the deriv
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2. Fundamentals δi error of satell
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2. Fundamentals Ionospheric refract
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2. Fundamentals 2.3.6.1 Ionosphere-
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2. Fundamentals Table 2.10: Linear
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3. Campaign Setup variable to the f
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3. Campaign Setup Figure 3.1: Examp
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3. Campaign Setup In this section w
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3. Campaign Setup 3.5 Processing Ov
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4. Import and Export of External Fi
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Page 168 and 169: 7. Parameter Estimation p u × 1 ve
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8. Initial Phase Ambiguities and Am
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9. Combination of Solutions 9.2 Seq
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9. Combination of Solutions Substit
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9. Combination of Solutions We may
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9. Combination of Solutions files a
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9. Combination of Solutions x x 1 t
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9. Combination of Solutions Both re
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9. Combination of Solutions 9.4 The
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9. Combination of Solutions 9.4.2 G
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9. Combination of Solutions Excepti
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9. Combination of Solutions As alre
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9. Combination of Solutions Table 9
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9. Combination of Solutions The poi
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9. Combination of Solutions (2) Tra
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9. Combination of Solutions Step 1:
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10. Station Coordinates and Velocit
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Page 220 AIUB Station coordinates a
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11. Troposphere Modeling and Estima
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12. Ionosphere Modeling and Estimat
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13. Differential Code Biases Promin
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13. Differential Code Biases Figure
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13. Differential Code Biases Figure
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13. Differential Code Biases ======
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13. Differential Code Biases Page 2
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14. Clock Estimation τ (BRUS-PTBB)
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14. Clock Estimation Here the limit
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14. Clock Estimation to zero. All c
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14. Clock Estimation #OBS : Number
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14. Clock Estimation 14.3 Clock RIN
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14. Clock Estimation cessed if CCRN
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14. Clock Estimation RINEX files th
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14. Clock Estimation the clock valu
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14. Clock Estimation SINGLE POINT P
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14. Clock Estimation Page 308 AIUB
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15. Estimation of Satellite Orbits
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16. Antenna Phase Center Offsets an
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17. Data Simulation Tool GPSSIM 17.
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17. Data Simulation Tool GPSSIM The
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17. Data Simulation Tool GPSSIM The
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17. Data Simulation Tool GPSSIM Res
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18. The Menu System 18.2 Starting t
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18. The Menu System 18.3.1 Menu Bar
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18. The Menu System 18.3.5 Panel Co
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18. The Menu System the menu the ne
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18. The Menu System Table 18.1: Pre
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18. The Menu System 18.5.3 System E
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18. The Menu System 18.7 Change Opt
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18. The Menu System 18.9 Technical
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18. The Menu System ... ! Environme
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18. The Menu System The keyword ENV
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18. The Menu System ! List of Remai
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18. The Menu System The MENUAUX-mec
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18. The Menu System Keyword values
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19. Bernese Processing Engine (BPE)
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20. Processing Examples inspect the
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20. Processing Examples 20.3.1 How
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20. Processing Examples • (option
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20. Processing Examples PID 111 PRE
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20. Processing Examples 20.4.1.4 Co
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20. Processing Examples 20.4.1.7 Cr
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20. Processing Examples 20.4.2.1 Co
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20. Processing Examples appears in
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20. Processing Examples PID 313 MPR
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20. Processing Examples Further rea
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20. Processing Examples # # Create
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20. Processing Examples PID 101 GPS
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20. Processing Examples The RINEX n
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20. Processing Examples # # Preproc
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20. Processing Examples the loop, d
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20. Processing Examples PID 903 CLK
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20. Processing Examples and IGS 00B
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20. Processing Examples • Save th
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20. Processing Examples PID 321 GPS
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20. Processing Examples PID 301 CLK
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21. Program Structure $C / %C% PGM
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21. Program Structure (program GPSE
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21. Program Structure continued fro
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21. Program Structure continued fro
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21. Program Structure ! -----------
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22. Data Structure "Program" Area $
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22. Data Structure Table 22.1: List
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22. Data Structure 22.4.2 Geodetic
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22. Data Structure 22.4.4 Antenna P
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Page 484 AIUB ANTENNA PHASE CENTER
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22. Data Structure 22.4.5 Satellite
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22. Data Structure 22.4.6 Satellite
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22. Data Structure DIFFERENCE OF GP
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22. Data Structure 22.4.9 Subdaily
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22. Data Structure EGM96 EGM96, VER
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22. Data Structure SINEX : OPTION I
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22. Data Structure 22.4.16 Panel Up
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22. Data Structure 22.6.2 Header an
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22. Data Structure 15 Antenna type(
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22. Data Structure SVN-NUMBER= 2 ME
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22. Data Structure -1 2 1 5 TITLE :
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22. Data Structure Used by: ORBGEN
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22. Data Structure 53064.00 53065.0
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22. Data Structure CODE’S MONTHLY
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22. Data Structure Table 22.4: Stat
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22. Data Structure (3) TYPE 003: HA
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22. Data Structure 22.8.4 Station P
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22. Data Structure Remarks: • Eac
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22. Data Structure The following st
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22. Data Structure Table 22.7: List
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22. Data Structure AJAC $$ FES2004
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22. Data Structure Station sigma fi
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22. Data Structure GOPE 11502M002 Z
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22. Data Structure 22.8.18 Receiver
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22. Data Structure CODE RAPID 3-DAY
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22. Data Structure 22.9.3 Meteo and
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22. Data Structure IONOSPHERE MODEL
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22. Data Structure 22.10 Miscellane
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22. Data Structure 22.10.4 Variance
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22. Data Structure 22.10.5 Normal E
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22. Data Structure 22.10.7 Observat
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22. Data Structure Created by: Each
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22. Data Structure ----------------
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22. Data Structure 22.10.17 BPE log
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23. Installation Guide 23.1.2 Conte
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23. Installation Guide 23.1.3.2 Ins
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23. Installation Guide BERN50 : $C
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23. Installation Guide If you have
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23. Installation Guide To make the
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23. Installation Guide List of Inst
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23. Installation Guide 23.2.4 Confi
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23. Installation Guide Configure me
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23. Installation Guide ${P}/EXAMPLE
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23. Installation Guide To recompile
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23. Installation Guide Page 574 AIU
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24. The Step from Version 4.2 to Ve
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BIBLIOGRAPHY Bock, H. (2004), Effic
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BIBLIOGRAPHY Janes, H. W., R. B. La
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BIBLIOGRAPHY Schaer, S. (1998), COD
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BIBLIOGRAPHY Page 588 AIUB
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INDEX OF PROGRAMS NEQ2ASC, 207, 541
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Index of Program Panels CODSPP 2: I
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Index of Program Panels MKCLUS 3: R
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INDEX OF KEYWORDS Antenna verificat
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INDEX OF KEYWORDS Cluster definitio
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INDEX OF KEYWORDS variance-covarian
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INDEX OF KEYWORDS orbit products, 1
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INDEX OF KEYWORDS Multi-session sol
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INDEX OF KEYWORDS Orbital elements
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INDEX OF KEYWORDS Receiver antenna
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INDEX OF KEYWORDS orbit modeling, 9
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INDEX OF KEYWORDS WGS-84, 19, 88, 2
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